| 注册
首页|期刊导航|火箭推进|应用功率谱法进行电磁阀线圈松动非线性模态仿真

应用功率谱法进行电磁阀线圈松动非线性模态仿真

廖云龙 吴佩沛 尤罡

火箭推进2023,Vol.49Issue(6):31-37,7.
火箭推进2023,Vol.49Issue(6):31-37,7.

应用功率谱法进行电磁阀线圈松动非线性模态仿真

Nonlinear modal simulation of solenoid valve coil looseness using power spectrum method

廖云龙 1吴佩沛 1尤罡1

作者信息

  • 1. 上海空间推进研究所,上海 201112||上海空间发动机工程技术研究中心,上海 201112
  • 折叠

摘要

Abstract

A nonlinear modal simulation method that combines time-domain transient dynamics simula-tion with frequency-domain power spectrum analysis was proposed.The simulation process is as follows:first,the periodogram method and probability statistics are used to simulate the random test conditions in the time domain.Combine and verify,obtain the fitting time domain conditions and prove the effective-ness,then use them as input conditions to conduct the transient dynamics simulation of the valve struc-ture,perform the power spectrum conversion on the time domain acceleration result curve,and finally ob-tain the structural nonlinear modal frequency through the power spectrum analysis.Different from the tra-ditional linear eigenvalue modal simulation principle,the nonlinear modal simulation method completes the nonlinear modal analysis through multiple processes of frequency domain power spectrum conditions-time domain fitting-time domain simulation-frequency domain analysis.The nonlinear effects of contact are introduced in the time domain simulation step.The thread loosening model of a certain solenoid valve coil uses conservative boundaries for linear modal simulation,and the deviation between simulation results and experimental results is 8.96%.After the friction coefficient calibration,the nonlinear modal frequen-cy simulation results and experimental deviation considering the nonlinear influence of contact are 0.69%.The result is better than linear simulation results.

关键词

非线性模态/功率谱密度/随机振动/瞬态动力学

Key words

nonlinear mode/power spectral density/random vibration/transient dynamics

分类

航空航天

引用本文复制引用

廖云龙,吴佩沛,尤罡..应用功率谱法进行电磁阀线圈松动非线性模态仿真[J].火箭推进,2023,49(6):31-37,7.

火箭推进

OA北大核心CSTPCD

1672-9374

访问量0
|
下载量0
段落导航相关论文